This International Standard defines the principles used to determine loads and the induced environment during the
service life of a space flight vehicle and its components, taking account of the notions of probability, combined
loads, corresponding safety factors and lifecycle.
Status: Under development
Technical Committee: ISO/TC 20/SC 14 Space systems and operations
- ICS :
This standard contributes to the following Sustainable Development Goal:
ISO/WD 14622Stage: 20.99
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